AIAA-2004-4939 The NASA Dryden AAR Project: A Flight Test Approach to an Aerial Refueling System
Min-Max Formulation for Heterogeneous Composite Plates with Thermal Residual Stresses
The simplest rectangular finite element for plate bending analysis
The Simplest Rectangular Finite Element for Plate Bending Analysis
Impact of Dynamics on the Design of the RL10B-2 Extendible Carbon-Carbon Exit Cone
Characterization and Comparison of Low Energy Impact Damage for Composite Plates